Chromium 33 vs. Nickel 600

Chromium 33 belongs to the otherwise unclassified metals classification, while nickel 600 belongs to the nickel alloys. They have 56% of their average alloy composition in common. There are 21 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.

For each property being compared, the top bar is chromium 33 and the bottom bar is nickel 600.

Chromium Alloy 33 (R20033)Nickel Alloy 600 (N06600, NA14)

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa		200
Elastic (Young's, Tensile) Modulus, GPa		190

Elongation at Break, %		45
Elongation at Break, %		3.4 to 35

Poisson's Ratio		0.27
Poisson's Ratio		0.29

Shear Modulus, GPa		81
Shear Modulus, GPa		75

Tensile Strength: Ultimate (UTS), MPa		850
Tensile Strength: Ultimate (UTS), MPa		650 to 990

Tensile Strength: Yield (Proof), MPa		430
Tensile Strength: Yield (Proof), MPa		270 to 760

Thermal Properties

Latent Heat of Fusion, J/g		320
Latent Heat of Fusion, J/g		310

Specific Heat Capacity, J/kg-K		480
Specific Heat Capacity, J/kg-K		460

Thermal Expansion, µm/m-K		14
Thermal Expansion, µm/m-K		13

Otherwise Unclassified Properties

Base Metal Price, % relative		36
Base Metal Price, % relative		55

Density, g/cm³		7.9
Density, g/cm³		8.5

Embodied Carbon, kg CO₂/kg material		6.0
Embodied Carbon, kg CO₂/kg material		9.0

Embodied Energy, MJ/kg		84
Embodied Energy, MJ/kg		130

Embodied Water, L/kg		250
Embodied Water, L/kg		250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m³		320
Resilience: Ultimate (Unit Rupture Work), MJ/m³		31 to 180

Resilience: Unit (Modulus of Resilience), kJ/m³		450
Resilience: Unit (Modulus of Resilience), kJ/m³		190 to 1490

Stiffness to Weight: Axial, points		14
Stiffness to Weight: Axial, points		13

Stiffness to Weight: Bending, points		25
Stiffness to Weight: Bending, points		23

Strength to Weight: Axial, points		30
Strength to Weight: Axial, points		21 to 32

Strength to Weight: Bending, points		25
Strength to Weight: Bending, points		20 to 26

Thermal Shock Resistance, points		21
Thermal Shock Resistance, points		19 to 29

Alloy Composition

Carbon (C), %		0 to 0.015
Carbon (C), %		0 to 0.15

Chromium (Cr), %		31 to 35
Chromium (Cr), %		14 to 17

Copper (Cu), %		0.3 to 1.2
Copper (Cu), %		0 to 0.5

Iron (Fe), %		25.7 to 37.9
Iron (Fe), %		6.0 to 10

Manganese (Mn), %		0 to 2.0
Manganese (Mn), %		0 to 1.0

Molybdenum (Mo), %		0.5 to 2.0
Molybdenum (Mo), %		0

Nickel (Ni), %		30 to 33
Nickel (Ni), %		72 to 80

Nitrogen (N), %		0.35 to 0.6
Nitrogen (N), %		0

Phosphorus (P), %		0 to 0.020
Phosphorus (P), %		0

Silicon (Si), %		0 to 0.5
Silicon (Si), %		0 to 0.5

Sulfur (S), %		0 to 0.010
Sulfur (S), %		0 to 0.015